View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00116U 26038.95777728 +.00000000 +00000-0 +80833-4 0 00008
2 00116 66.8077 207.0453 0075407 358.6421 1.4441 13.92305851 08
| Epoch (UTC): | 07 February 2026 22:59:11 |
| Eccentricity: | 0.0075407 |
| inclination: | 66.8077° |
| perigee height: | 866 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 207.0453° |
| argument of perigee: | 358.6421° |
| revolutions per day: | 13.92305851 |
| mean anomaly at epoch: | 1.4441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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